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In-flight refueling system, damping device and method for damping oscillations in in-flight refueling system components

机译:空中加油系统,阻尼装置和用于衰减空中加油系统组件中的振动的方法

摘要

An in-flight refueling system, damping device and method are provided for substantially reversing a change in the disposition of an elongate hose extending from a first aircraft during an in-flight refueling operation. The various embodiments of the present invention provide a compact, lightweight, and easily installed damping device that may act to minimize the occurrence of oscillations within the elongate hose that may act to produce a change in the disposition of the elongate hose. In addition, the embodiments of the present invention facilitate the detuning of the elongate hose and, for instance, an attached drogue that may oscillate uncontrollably at a resonant frequency in response to aerodynamic forces exerted on the hose and drogue during an in-flight refueling operation.
机译:提供一种飞行中加油系统,阻尼装置和方法,以在飞行中加油操作期间基本反转从第一飞机延伸的细长软管的布置变化。本发明的各种实施例提供了紧凑,轻便且易于安装的阻尼装置,其可用于使细长软管内的振动的发生最小化,该振动可用于引起细长软管的布置的改变。另外,本发明的实施例促进了细长软管的失谐,例如,附接的锥套可能在飞行中加油操作期间响应于施加在软管和锥套上的空气动力而以共振频率失控地振荡。 。

著录项

  • 公开/公告号US7198229B2

    专利类型

  • 公开/公告日2007-04-03

    原文格式PDF

  • 申请/专利权人 STEVEN B. SCHROEDER;

    申请/专利号US20060353276

  • 发明设计人 STEVEN B. SCHROEDER;

    申请日2006-02-13

  • 分类号B64D39/00;

  • 国家 US

  • 入库时间 2022-08-21 21:01:06

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